INTELSAT 25(PROTOSTAR 1)
Informationen über den Satelliten. INTELSAT 25(PROTOSTAR 1) - INTELSAT 25 (IS-25)
| Name im Katalog Spacetrack | INTELSAT 25(PROTOSTAR 1) |
| Alternative Bezeichnung | INTELSAT 25 (IS-25) |
| Gruppe | INTELSAT |
| In die Umlaufbahn bringen |
2008-07-07 |
| Deorbitation |
|
| Herkunftsland/-organisation | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. | FRGUI (Guiana Space Centre, French Guiana) |
| Typ | Satellit |
| Kategorie | |
| Perygeum | 35773 km |
| Apogäum | 35800 km |
| Höhe INTELSAT 25(PROTOSTAR 1) | 35875.31 km |
Informationen über INTELSAT 25(PROTOSTAR 1)
INTELSAT 25 (IS-25), also known as Protostar 1, is a communication satellite owned by PROTO and operated for communication purposes. It was launched on July 7, 2008, from ELA3 launch pad at the Guiana Space Centre using an Ariane 5ECA launch vehicle. The spacecraft measures 6.2 meters in length, 2.4 meters in diameter, and has a span of 31.1 meters. It has a dry mass of 1774 kilograms and a launch mass of 4194 kilograms. Equipped with the FS-1300 bus configuration and SSL-1300 design, IS-25 features 16 (+6) Ku-band transponders and 36 (+2) C-band transponders for communication services. It is powered by two deployable solar arrays and batteries, manufactured by LOR, with a designed lifetime of 17 years. The satellite has a shape described as Box + 2 Pan + Dish and an RCS (Reflective Coefficient Surface) value of 12.685.
der Satellit INTELSAT 25(PROTOSTAR 1) hinausgetragen 07.07.2008r. Durchschnittshöhe INTELSAT 25(PROTOSTAR 1) Text Nummer 1: das. 35875.31 km. Durchschnittsgeschwindigkeit INTELSAT 25(PROTOSTAR 1) beträgt 11057.34 km/h. Neigung INTELSAT 25(PROTOSTAR 1) Satelliten 2.35°.Durchschnittshöhe der Orbitalbahn. INTELSAT 25(PROTOSTAR 1)
Durchschnittsgeschwindigkeit INTELSAT 25(PROTOSTAR 1)
Durchschnitt INTELSAT 25(PROTOSTAR 1)
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